NVAMediumJEE 2025Elasticity & Stress-Strain Curve

JEE Physics 2025 Question with Solution

Two slabs with square cross section of different materials (1,2)(1,2) with equal sides (l)(l) and thickness d1\mathrm{d}_{1} and d2\mathrm{d}_{2} such that d2=2 d1\mathrm{d}_{2}=2 \mathrm{~d}_{1} and l>d2l>\mathrm{d}_{2}. Considering lower edges of these slabs are fixed to the floor, we apply equal shearing force on the narrow faces. The angle of deformation is θ2=2θ1\theta_{2}=2 \theta_{1}. If the shear moduli of material 11 is 4×109 N/m24 \times 10^{9} \mathrm{~N} / \mathrm{m}^{2}, then shear moduli of material 22 is x×109 N/m2\mathrm{x} \times 10^{9} \mathrm{~N} / \mathrm{m}^{2}, where value of x is _____ .

Answer

Correct answer:1

Step-by-step solution

Standard Method

Given: Two slabs of materials 11 and 22 have equal side ll, thicknesses d1d_1 and d2d_2 with d2=2d1d_2 = 2d_1. Equal shearing force FF is applied on the narrow faces, and the deformation angles satisfy θ2=2θ1\theta_2 = 2\theta_1. Shear modulus of material 11 is η1=4×109N/m2\eta_1 = 4 \times 10^9 \, \text{N/m}^2.

Find: The value of xx in η2=x×109N/m2\eta_2 = x \times 10^9 \, \text{N/m}^2.

Using the relation from the solution working:

2θ1=θ22\theta_1 = \theta_2 2σ1η1=σ2η22 \frac{\sigma_1}{\eta_1} = \frac{\sigma_2}{\eta_2}

For equal shearing force on narrow faces, the shear stresses are

σ1=Fld1,σ2=Fld2\sigma_1 = \frac{F}{l d_1}, \qquad \sigma_2 = \frac{F}{l d_2}

Substituting these into the strain relation,

2(Fld1η1)=Fld2η22\left(\frac{F}{l d_1 \eta_1}\right) = \frac{F}{l d_2 \eta_2}

Given d2=2d1d_2 = 2d_1,

2(Fld1η1)=F2ld1η22\left(\frac{F}{l d_1 \eta_1}\right) = \frac{F}{2l d_1 \eta_2}

Cancelling common factors,

η2=η14\eta_2 = \frac{\eta_1}{4}

Now substitute η1=4×109N/m2\eta_1 = 4 \times 10^9 \, \text{N/m}^2:

η2=1×109N/m2\eta_2 = 1 \times 10^9 \, \text{N/m}^2

Hence,

x=1x = 1

Therefore, the value of xx is 11.

Detailed Ratio Method

Given: θ2=2θ1\theta_2 = 2\theta_1, d2=2d1d_2 = 2d_1, and G1=4×109N/m2G_1 = 4 \times 10^9 \, \text{N/m}^2.

Find: G2=x×109N/m2G_2 = x \times 10^9 \, \text{N/m}^2.

For shear deformation,

G=shear stressshear strainG = \frac{\text{shear stress}}{\text{shear strain}}

so

θ=shear stressG\theta = \frac{\text{shear stress}}{G}

Since the force is the same but the narrow face areas are different,

τ1=Fld1,τ2=Fld2\tau_1 = \frac{F}{l d_1}, \qquad \tau_2 = \frac{F}{l d_2}

Therefore,

θ1=Fld1G1,θ2=Fld2G2\theta_1 = \frac{F}{l d_1 G_1}, \qquad \theta_2 = \frac{F}{l d_2 G_2}

Using θ2=2θ1\theta_2 = 2\theta_1,

Fld2G2=2(Fld1G1)\frac{F}{l d_2 G_2} = 2\left(\frac{F}{l d_1 G_1}\right)

Substitute d2=2d1d_2 = 2d_1:

F2ld1G2=2Fld1G1\frac{F}{2l d_1 G_2} = \frac{2F}{l d_1 G_1}

Cancelling Fld1\frac{F}{l d_1},

12G2=2G1\frac{1}{2G_2} = \frac{2}{G_1} G2=G14G_2 = \frac{G_1}{4}

Now,

G2=4×1094=1×109N/m2G_2 = \frac{4 \times 10^9}{4} = 1 \times 10^9 \, \text{N/m}^2

So the required value is x=1x = 1.

Common mistakes

  • Assuming the shear stress is the same for both slabs because the applied force is equal. This is wrong because the force acts on narrow faces of areas ld1l d_1 and ld2l d_2, which are different. Use τ=FA\tau = \frac{F}{A} separately for each slab.

  • Using θ1G\theta \propto \frac{1}{G} directly without accounting for thickness-dependent face area. This misses the fact that stress depends on dd here. First write θ=τG=FldG\theta = \frac{\tau}{G} = \frac{F}{l d G} and then compare ratios.

  • Substituting d2=2d1d_2 = 2d_1 incorrectly and concluding G2=G1G_2 = G_1. The thickness appears in the denominator of stress, so careful algebra is required. After substitution, solve the full equation before cancelling terms.

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